Joint Aviation Authorities JAA AEROPLANE DATA SHEET JAA/25/99-022 Issue 4 DHC-8 Series 400 Variants DHC-8-401 DHC-8-402 Manufacturer: Bombardier Inc. 123 Garratt Boulevard Downsview, Ontario M3K 1Y5 JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 1 of 8
CONTENT I. General II. III. IV. Certification Basis Technical Characteristics and Operational Limitations Operating and Service Instructions V. Notes JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 2 of 9
I General 1 Data Sheet No.: JAA/25/99-022 Issue: 4 Date: 09 November 2001 2. Type: DHC-8 Series 400 3. Variants: DHC-8-401 DHC-8-402 4. Airworthiness Category: Transport Category 5. Performance Category: JAR OPS Performance Group A Category 6. Transport Canada Bombardier Inc. Type Certificate Holder: 123 Garratt Boulevard Downsview, Ontario M3K 1Y5 7. Manufacturer: Bombardier Inc. 123 Garratt Boulevard Downsview, Ontario M3K 1Y5 8. JAA Validation Application Date: 31 January 1995 9. JAA Validation Recommendation Date: 26 November 1999 II Certification Basis 1. Reference Application Date for Transport Canada Certification: 31 January 1995 2. Transport Canada Certification Date: DHC-8-401 03 August 1999 DHC-8-402 04 August 1999 Transport Canada Type Certificate Data Sheet No. DHC-8-401/ DHC-8-402 A-142 Issue 20 or later revision 3. Transport Canada Certification Basis: as defined in Transport Canada Type Certificate Data Sheet No. A-142 4. JAA Airworthiness Requirements: (a) JAR 25 Change 14 5. Elect to comply with (b) JAR 25 Amendment 25/96/1 (c) JAR AWO Change 2 JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 3 of 9
Procedural Codes: (a) JAR 1 Definitions Change 4 (b) JAR 21 Change 1 6. JAA Special Conditions: (a) CRI C-01 Yawing Maneuvering Conditions INT/POL/25/8 Issue 1 (b) CRI D-01 (c) CRI F-01 (d) CRI F-02 (e) CRI F-03 (f) CRI G-07 Worn Brakes INT/POL/25/6 Issue 1 Protection from the Effects of HIRF INT/POL/25/2 Issue 1 Protection from the Effects of Lightning Strike- Direct Effects INT/POL/25/3 Issue 1 Protection from the Effects of Lightning Strike- Indirect Effects INT/POL/25/4 Issue 2 Steep Approach Landing Capability (SAL) 7. JAA Exemptions: None 8. JAA Equivalent Safety Findings: (a) CRI B-04 Stall Warning and Stall Warning Speeds and Maneuver Capability (JAR 25.103,107,119,125,143 and 207) (b) CRI C-04 (c) CRI D-10 (d) CRI D-02 (e) CRI G-04 Flutter, Deformation and Failsafe Criteria (JAR 25.629) Nose-Wheel Steering System Protection {JAR 25X745(d)} Hydraulic System Proof Testing {JAR 25.1435(b)(1)} Accelerate Stop Distance INT/POL/25/5 Issue 1 (JAR 25.109) 9. JAA Environmental Standards: Noise: ICAO Annex 16, 3 rd Edition, Volume 1, (for details refer to CRI A-03) Chapter 3, Amendment 5 Maximum Noise Levels *) Take-off 78,3 EPNdB (flap 5 ) Sideline 84,1 EPNdB (flap 5 ) Approach 94,3 EPNdB (flap 35 ) 94,9 EPNdB (flap 15 ) *) for specific noise levels for maximum weights as listed in Section III/13 refer to AFM PSM 1-84-1A. Engine Emissions: ICAO Annex 16, 2 nd Edition, Volume 2 JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 4 of 9
10. For Additional National Design Requirements (ANDRs) as specified in JAA Administrative and Guidance Material, Section 3/ Part 4: Registers or as otherwise defined by National Aviation Authorities refer to CRI A-02. III Technical Characteristics and Operational Limitations 1. Design Standard: Current Issue of AEROC 8.1.AC.1 - Definition of Certified Airplanes 2. Description: Detail Specification No. DS8-400B 3. Equipment: Equipment register 4. Dimensions: Wingspan: 28,4 m (93 ft 3 in) Length: 32,8 m (107 ft 9 in) Height: 8,3 m (27 ft 5 in) Wing area: 63,1 m² (679 ft²) 5. Engines: 2 Pratt & Whitney Canada Engines Model PW 150 A JAA Data Sheet No. JAA / E / 98-019 5.1 Engine Limits: for details refer to AFM - PSM 1-84-1A 6. Auxiliary Power Unit (APU): 1 Hamilton Sundstrand Power Systems APS 1000 T-62T-46C12 TSO authorization, dated 23 July 1999 Note: Option only 6.1 APU Limits: for details refer to AFM - PSM 1-84-1A 7. Propellers: 2 Dowty Aerospace Propellers Model R408/6-123-F/17 JAA Data Sheet No. JAA / P / 99-001 7.1 Propeller Limits: Blade Diameter 4,11 m (13,5 ft) Pitch settings at 0,70 radius: Feather Flight fine (Electronic) Flight fine (Hydraulic) Ground fine Full reverse 84,5 o 16,5 o 16,0 o -3,5 o -19,0 o 8. Fuel: Propeller (N P ) Take-off 1.020 rpm Max. continuous 1.020 rpm 8.1 Eligible Fuels: Kerosene Jet A, A-1, JP-5, JP-8 Wide Cut Jet B, JP-4 8.2 Fuel Capacity: kg lbs Liters Imp. Gals Usable 5.318 11.724 6.526 1.436 Unusable 73 160 89 20 JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 5 of 9
9. Oil: Total 5.391 11.884 6.615 1.456 9.1 Eligible Oils: Oils conforming to specification MIL-L-23699 (for details refer to AFM - PSM 1-84-1A) 9.2 Oil Capacity Liters Imp. Gals per Engine: Usable 5,6 1,23 Total 24,9 5,48 10. Air Speeds: Knots (IAS) V MO *) (Maximum Operating) 0 to 8.000 ft 245 10.000 ft 282 18.000 ft 286 20.000 ft 275 25.000 ft 248 *) V MO various linearly between given altitudes V FE (Flaps extended) Flap 5 o 200 Flap 10 o 181 Flap 15 o 172 Flap 35 o 158 V VA (Maneuvering) 204 V RA (Rough Air) 210 V LO (Landing Gear Operation) 200 V LE (Landing Gear extended) 215 11. Maximum Operating Altitude: (for other airspeeds refer to AFM - PSM 1-84-1A) 7.620 m (25.000 ft) (Pressure altitude) 12. All Weather Capability: CAT II 13. Maximum Weights: kg lb DHC-8-401& 402 Taxi and Ramp 28.077 61.900 (with MODSUM 4-201539 Take-off 27.987 61.700 incorporated) Landing 27.442 60.500 Zero Fuel 25.174 55.500 DHC-8-401& 402 Taxi and Ramp 29.089 64.130 (with MODSUM 4-308807 Take-off 28.998 63.930 incorporated) Landing 28.009 61.750 Zero Fuel 25.855 57.000 DHC-8-401& 402 Taxi and Ramp 29.347 64.700 (with MODSUM 4-308907 Take-off 29.257 64.500 incorporated) Landing 28.009 61.750 Zero Fuel 25.855 57.000 14. Center of Gravity Range: 13,8 % to 36,0 % (MAC) Landing Gear down 10,8 % to 40,0 % (MAC) In Flight: Landing Gear up JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 6 of 9
15. Reference Datum: Plate located on centerline at Station 428,0 in (1087,1 cm) on underside of fuselage. 16. Mean Aerodynamic Cord (MAC): 2,400 m (7,876 ft) 17. Leveling Means: Plumb bob and target in RH emergency exit opening. 18. Minimum Flight Crew: 2 (Pilot and Copilot) 19. Maximum Passenger Seating Capacity: DHC-8-401 70 passengers (refer to Note 1) DHC-8-402 78 passengers 20. Exits: No. Type Size 1 II / III **) 20 x 56 inches 1 I 27 x 70 inches 1 I 27 x 56 inches 1 I 30 x 70 inches **) Type III exit for showing compliance with JAR 25.801 only. 21. Baggage / Cargo Compartments: Class Maximum Volume Max. allowable Load ***) Front C 2,58 m³ (91 ft ³) 413 kg (910 lb) Aft C 11,64 m³ (411 ft ³) 1.669 kg (3.680 lb) ***) for individual aeroplane configurations refer to AFM PSM 1-84-1A 22. Wheels and Tires: Tricycle landing gear, retractable, dual side by side wheel type. Main wheels sized to accept 32 x 8,8-16 or 34 x 8,8-16 tires. Nose gear sized to accept 22 x 6,5-10 tires. IV Operating and Service Instructions ****) 1. Operating Instructions: 1.1 Airplane Flight Manual PSM 1-84-1A (DHC-8-401 or DHC-8-402) 1.2 Airplane Operating Manual PSM 1-84-1 1.3 Weight and Balance Manual PSM 1-84-8 1.4 Master Minimum Equipment List PSM 1-84-16A 1.5 MMEL Procedures Manual PSM 1-84-16 2. Service Instructions: 2.1 Airplane Maintenance Manual PSM 1-84-2 2.2 Maintenance Requirements Manual PSM 1-84-7 Part 1: MRB Report Part 2: Airworthiness Limitation Items (ALIs) a) Certification Maintenance Requirements (CMRs) b) Structural Maintenance Program c) System Safe life Components issued on 4 Nov. 1999 or later issued on 4 Nov. 1999 or later 2.3 Service Letters and Service Bulletins (refer to Publication Index) 2.4 Structural Repair Manual PSM 1-84-3 JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 7 of 9
2.5 Cargo Loading PSM 1-84-8A 2.6 Illustrated Parts Manual PSM 1-84-4 2.7 Task Cards Manual PSM 1-84-7 TC ****) With exemption of Airplane Flight Manual PSM 1-84-1A all instructions are applicable to the DHC-8 Series 400. V Notes 1. Cabin Interior and Seating Configurations must be approved and are listed in AEROC 8.1.AC.1.Sect. 400, current Issue. JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 8 of 9
Anhang 1 zum LBA-Gerätekennblatt Nr. 2868 DHC-8 Series 400 Ausgabe 2 Datum: 22.11.2001 Seite 1 von 1 Ergänzungen und Beschränkungen des LBA-Gerätekennblattes 2868: 1. Dieses LBA-Gerätekennblatt besteht aus einem Deckblatt, dem JAA Data Sheet Nr. JAA/25/99-022 und dem Anhang 1 Ergänzungen und Beschränkungen des LBA- Gerätekennblattes 2868 in der jeweils letztgültigen Ausgabe. 2. Für die Musterprüfung und die Musterbetreuung der DHC-8 Series 400 im JAA-Bereich ist das JAA-Team unter Leitung eines federführenden Musterprüfers (PCM) der Austro Control zuständig; die Zulassung aller Änderungen erfolgt nach den zwischen der JAA, des TCA und Bombardier vereinbarten Verfahren für die Betreuung des Musters nach erteilter Musterzulassung (Post Type Validation Procedures). 3. Das Triebwerk PW 150 A verfügt gemäß 1 (1) LuftVZO gemäß dem LBA-Gerätekennblatt Nr. 7034 über eine eigene LBA-Zulassung. 4. Der Propeller von Dowty Aerospace, Model R408/6-123-F/17 verfügt über eine eigene LBA- Zulassung, LBA-Gerätekennblatt Nr. 32.130/98. 5. Die Hilfskraftturbine (APU) Hamilton Sundstrand Power Systems APS 1000 T-62T-46C12 verfügt gemäß 1 (1) LuftVZO über eine eigene LBA-Zulassung, LBA.N-O.6608 JTSO. 6. Eine LBA-Lärmzulassung besteht nur für die Baureihen DHC-8-401 und DHC-8-402 mit den Maximum Weights (siehe Punkt III.13 des Gerätekennblatts 2868, Issue 4) Taxi and Ramp 29.347 kg with MODSUM 4-308907 Take-Off 29.257 kg Landing 28.009 kg. Für die weiteren im JAA Data Sheet aufgeführten Gewichtsklassen (Punkt III.13) besteht keine LBA-Zulassung. ---ENDE--- JAA Data Sheet 25/99-022 Issue 4 (09.11.2001) Page 9 of 9